针对导弹分导或多星发射中时序分离方式的不足,提出了一种让反推分离力同时参与闭环的组合控制策略及分离方法.通过建立分离动力学模型,运用MATLAB/Simulink软件对分离过程进行了数值仿真,并与最佳时序分离方法进行了比较,仿真结果表明反推分离力参与闭环的组合控制策略,在鲁棒性、方便性和安全性方面更有优越性,实现简单,在导弹分导与多星发射分离中具有参考和应用价值.
For the shortage of the timing control for the separation of sub-guided missile or multi-satellite, a new closedloop control method based on thrust reverser was proposed. The model of separation was established and simulated by MATLAB/Simulink, and the two methods were compared. Simulation results indicate that the new control method is more robust, more convenient and safer. It has reference and value in the separation of subguided missile or multi-satellite.
郝子龙,刘新建.多弹头导弹反推分离的一种组合控制方法[J].动力学与控制学报,2015,13(3):205~209; Hao Zilong, Liu Xinjian. A combined control strategy for separation of mirv with reaction thrust[J]. Journal of Dynamics and Control,2015,13(3):205-209.
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